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AIRCRAFT CONFIGURATION
This section is provided as a reference to the pilot for a record of the
configuration of the KFD 840 as it is installed in the aircraft
ITEM
RESOL-
UTION
Roll
Adjust
Pitch
Adjust
S/R
Pointer
V
S0
V
S1
V
FE
V
NO
V
NE
V
MCA
V
YSE
KFD 840 PG PN 7450-0840-01
Rev C May 28, 2010
©
Honeywell International Inc. Do not copy without express permission of Honeywell
Honeywell Bendix/King KFD 840 Primary Flight Display
INPUT
VALUE
RANGE
0.1
0-180.0
0.1
0-90.0
--
SKY,
ROLL
1.0
0-240
(276)
1.0
0-240
(276)
1.0
0-240
(276)
1.0
0-240
(276)
1.0
0-240
(276)
1.0
0-240
(276)
1.0
0-240
(276)
UNITS
CONFIGURATION
DEG
DEG
--
Kts /
(MPH)
Kts /
(MPH)
Kts /
(MPH)
Kts /
(MPH)
Kts /
(MPH)
Kts /
(MPH)
Kts /
(MPH)
Appendix
11-3
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